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B737 Flashcards

1
Q

Wind shear (manual flight)

A

“Wind shear, TOGA”
A/p off
TOGA switch push
Aggressively apply maximum thrust
A/t off
Wings level
Pitch 15 degrees
Speedbrakes retracted
Follow f/d go around commands
Maintain configuration
Monitor v/s
Monitor altitude

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2
Q

Wind shear (auto flight)

A

“Windshear, TOGA”
Push TOGA switch
Verify TOGA mode
Verify TOGA thrust
Retract speed brakes
Monitor performance
Maintain configuration
Monitor v/s and altitude

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3
Q

Engine failure in cruise and drift down

A

PF
“Disengage autothrottle, set max continuous thrust” (pm actions)
Trim
Confirm max continuous thrust
“Engine out page” (pm selects e/o page, sets e/o alt and speed on mcp)
-at e/o speed select LVL change (pm = lights on & advise ATC)
Turn if required
“Checklist, engine failure” (pm actions checklist)
At level off: determine optimum altitude
Adjust thrust
Land at nearest suitable airport

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4
Q

T/A

A

Look for traffic
Manoeuvre as needed

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5
Q

TCAS RA

A

A/p off
A/t off
Pitch to satisfy RA command
(If in landing configuration: max thrust, flaps 15 and gear up with positive rate)
PM-lights on

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6
Q

Nose high

A

Recognize
A/p off
A/t off
Nose down elevator
Nose down trim (if required)
Reduce thrust
Bank to lower nose (if required)
At horizon: wings level
Adjust thrust
Adjust pitch

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7
Q

Nose low recovery

A

Recognize
A/p off
A/t off
Recover from stall
Wings level
Nose up
Adjust thrust and drag

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8
Q

GPWS caution

A

Correct flight path or condition

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9
Q

GPWS warning

A

“Firewall”
A/P off
A/T off
Aggressively apply max thrust
Pitch 20 degrees
Retract speedbrakes
(Pitch to PLI/shaker if needed)
Maintain configuration
Monitor RA
Accelerate when clear

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10
Q

Overrun warning (airborne)

A

Go around

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11
Q

Overrun warning (ground)

A

Reject takeoff….

Thrust idle
Max brakes
Speedbrakes up
Max reverse

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12
Q

Stall

A

“Stall”
Hold control column firmly
A/P off
A/T off
Pitch nose down
Recovery:
Wings level
Add thrust
Retract Speedbrakes
Maintain configuration (if on t/o and clean, call “flaps 1”)
Adjust thrust
Establish pitch attitude
Return to flight path

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13
Q

Windshear indications (5 + 4 on HUD)

A

+/-15kts
+/-500fpm v/s
5 degrees of pitch
1 dot displacement
Unusual thrust
HUD:
Erratic wind vector
Rapid changes to flight path
Opposing acceleration and airspeed vectors
Large differences between airspeed and ground speed

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14
Q

Ground incident

A

“Remain seated, remain seated”
“Incharge flight attendant call/report to the flight deck”
“Checklist, passenger evacuation”

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15
Q

Aborted engine start

A

Engine start lever cutoff

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16
Q

Engine limit/surge/stall

A

A/T off
Thrust lever- confirm and retard until condition stops

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17
Q

Loss of thrust on both engines

A

Engine start switches (both) - flight
Start levers (both) - cutoff
When EGT decreases:
Start levers (both) - idle
Repeat as needed

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18
Q

Apu fire

A

Apu fire switch - confirm, pull, and rotate (hold for 1 sec)
Apu switch - off

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19
Q

Engine overheat

A

A/T off
Thrust lever - confirm and close

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20
Q

Smoke/fire from a lithium battery

A

Transfer control (if necessary)
“Backup to the flight deck, backup to the flight deck”

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21
Q

Smoke/fire/fumes

A

Oxygen masks on
Communications establish

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22
Q

Runaway stabilizer

A

Hold control column firmly
A/P off
A/T off
Control aircraft with pitch and thrust
Use electric stab trim
If runaway stops with A/P disconnect: do not re-engage A/P
If runaway continues: stab trim cutout switches-cutout
If runaway continues: hold trim wheel

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23
Q

Unreliable airspeed

A

A/P off
A/T off
F/D off
Power & Pitch: flaps extended = 80% and 10 degrees
Flaps up = 75% and 4 degrees

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24
Q

Landing configuration horn

A

Ensure correct configuration

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25
Q

Warning horn (intermittent)
-or-
warning: takeoff/cabin altitude/takeoff configuration
(Above 10,000’ & on the ground)

A

Above 10,000’ : masks don
Communications establish
On ground: ensure correct t/o configuration

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26
Q

Crew incapacitation

A

Assume control
A/P on
Tilt back
Slide back
Restrain
Remove/replace

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27
Q

Oceanic diversion (all engines)

A

Initiate drills and time critical checklists
Declare emergency and request clearance
Follow clearance
-or-
Turn 30 degrees R/L
Offset 5NM
Altitude +/-500’

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28
Q

Oceanic diversion (single engine)

A

Complete drills and time critical checklists
Declare emergency and request clearance
Follow clearance
-or-
Turn 30 degrees R/L
Offset 5NM
When offset, descend below FL290 +/-500’

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29
Q

Fuel burn in flight (kg/min)

A

36kg/min

30
Q

Apu fuel burn (ground/flight)

A

107kg/hr ground
45kg/hr FL390

31
Q

Takeoff alternate (mins & distances)

A

60min/343NM
120min/688 NM

32
Q

Heading tolerance b/w captain and f/o

A

+/- 4 degrees

33
Q

Altimeter tolerances

A

CA-FO = 50’
From field elevation = 75’

34
Q

Passenger count tolerances

A

+/- 3 per zone
+/- 6 total

35
Q

Definition of Icing conditions

A

10 degrees or below
Visible moisture (1sm or less)

36
Q

Run up required….

A

+3 or below
Visible moisture
50% N1 every 60 minutes
50% N1 for 5 seconds before takeoff

37
Q

Minimum oil temp for takeoff

A

31C

38
Q

Tailstrike pitch

A

11 degrees

39
Q

Reject before 80kts for…(10)

A

activation of the master caution system
• system failure(s)
• unusual noise or vibration
• tire failure
• abnormally slow acceleration
• take-off configuration warning
• fire or fire warning
• engine failure
• predictive windshear warning
• if the airplane is unsafe or unable to fly

40
Q

Reject after 80kts for…(4)

A

• fire or fire warning
• engine failure
• predictive windshear warning
• if the airplane is unsafe or unable to fly

41
Q

Notify load if fuel out by ———-kgs

A

300kgs or more

42
Q

Max rate of climb

A

Flaps up speed + 50kts or 0.78M

43
Q

ETOPS 180 minutes distance

A

1146NM

44
Q

Maximum tailwind for t/o and landing

A

15kts

45
Q

Vfe 1 & 5

A

250kts

46
Q

Vfe 10

A

210kts

47
Q

Vfe 15

A

200kts

48
Q

Vfe 25

A

190kts

49
Q

Vfe 30

A

175kts

50
Q

Vfe 40

A

166kts

51
Q

Vlo retract

A

235kts

52
Q

Vlo extend

A

270kts

53
Q

Vle

A

320 kts

54
Q

Max diff

A

9.1 psi

55
Q

Max auto land headwind/crosswind/tailwind

A

25/15/10

56
Q

Max/min glideslope angle for autoland

A

3.25/2.5

57
Q

Max altitude with flaps extended

A

20000’

58
Q

Max fuel imbalance

A

453kg

59
Q

Max altitude for APU bleed and electrical load

A

10000’

60
Q

Max altitude for APU bleed (no electrical load)

A

17000’

61
Q

Max altitude for APU electrical load only (no bleed)

A

41000’

62
Q

Minimum oil temperature for start

A

-40C

63
Q

Engine ignition must be continuous for….(4)

A

Moderate to heavy freezing rain
Hail
Sleet

64
Q

Max oil temp

A

155 for 15 minutes
140 continuous

65
Q

Turbulence penetration speed

A

280/M0.76

66
Q

Maximum Amount of Snow or Slush for Take-off

A

4” dry snow
1/2” wet snow/slush/standing water

67
Q

Wingspan

A

117’ 10”

68
Q

Turn radius

A

80’

69
Q

Cargo fire suppression time: etops and non-etops

A

Etops - 3h15
Non-etops - 1h15

70
Q

ETOPS diversion times & distances (non-ETOPS, 120mins, 180mins)

A

Non-ETOPS - 395
120mins-764NM
180mins-1146

B737 (1 decks)

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